▸Orbital parameters

Orbit class	SSO
Inclination	97.5801°
Eccentricity	0.0001127
Period	96.4 min
Apogee	587 km
Perigee	585 km
Mean motion	14.93789658 rev/day
RAAN	61.9307°
Arg of perigee	81.8545°
Mean anomaly	278.2803°
B*	2.6137e-4
Rev at epoch	64,070

▸Two-line element set (TLE)

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

1 40013U 14033D 26188.14531919 .00002717 00000-0 26137-3 0 9996

2 40013 97.5801 61.9307 0001127 81.8545 278.2803 14.93789658640705

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DEIMOS-2",
  "OBJECT_ID": "2014-033D",
  "EPOCH": "2026-07-07T03:29:15.578+00:00",
  "MEAN_MOTION": 14.93789658,
  "ECCENTRICITY": 0.0001127,
  "INCLINATION": 97.5801,
  "RA_OF_ASC_NODE": 61.9307,
  "ARG_OF_PERICENTER": 81.8545,
  "MEAN_ANOMALY": 278.2803,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40013,
  "REV_AT_EPOCH": 64070,
  "BSTAR": 0.00026137,
  "MEAN_MOTION_DOT": 0.00002717,
  "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	DEIMOS-2
Operator	Elecnor Deimos (Castilla-La Mancha)HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree UrtheCastMEDIUMvia Wikidata
Country	Spain
Launch date	Jun 19, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia GCAT — Jonathan McDowell's General Catalog⚠

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/40013

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