▸Orbital parameters

Orbit class	SSO
Inclination	97.4578°
Eccentricity	0.0010014
Period	95.3 min
Apogee	542 km
Perigee	528 km
Mean motion	15.10336335 rev/day
RAAN	177.7702°
Arg of perigee	334.7729°
Mean anomaly	25.3010°
B*	1.2618e-4
Rev at epoch	68,940

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 39419U 13066D 26188.14631398 .00002008 00000-0 12618-3 0 9993

2 39419 97.4578 177.7702 0010014 334.7729 25.3010 15.10336335689408

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DUBAISAT-2",
  "OBJECT_ID": "2013-066D",
  "EPOCH": "2026-07-07T03:30:41.528+00:00",
  "MEAN_MOTION": 15.10336335,
  "ECCENTRICITY": 0.0010014,
  "INCLINATION": 97.4578,
  "RA_OF_ASC_NODE": 177.7702,
  "ARG_OF_PERICENTER": 334.7729,
  "MEAN_ANOMALY": 25.301,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39419,
  "REV_AT_EPOCH": 68940,
  "BSTAR": 0.00012618,
  "MEAN_MOTION_DOT": 0.00002008,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	DUBAISAT-2
Operator	Emirates Institution for Advanced Science and TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Mohammed bin Rashid Space CentreMEDIUMvia Wikidata
Country	United Arab Emirates
Launch date	Nov 21, 2013HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/39419

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.