▸Orbital parameters

Orbit class	SSO
Inclination	97.7608°
Eccentricity	0.0044969
Period	97.3 min
Apogee	662 km
Perigee	599 km
Mean motion	14.79569333 rev/day
RAAN	333.3885°
Arg of perigee	11.0111°
Mean anomaly	349.2075°
B*	7.4507e-5
Rev at epoch	64,899

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40016U 14033G 26187.93411649 .00000515 00000-0 74507-4 0 9991

2 40016 97.7608 333.3885 0044969 11.0111 349.2075 14.79569333648996

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SAUDISAT 4",
  "OBJECT_ID": "2014-033G",
  "EPOCH": "2026-07-06T22:25:07.665+00:00",
  "MEAN_MOTION": 14.79569333,
  "ECCENTRICITY": 0.0044969,
  "INCLINATION": 97.7608,
  "RA_OF_ASC_NODE": 333.3885,
  "ARG_OF_PERICENTER": 11.0111,
  "MEAN_ANOMALY": 349.2075,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40016,
  "REV_AT_EPOCH": 64899,
  "BSTAR": 0.000074507,
  "MEAN_MOTION_DOT": 0.00000515,
  "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	SAUDISAT 4
Operator	King Abdul Aziz City for Science and TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree King Abdulaziz City for Science and TechnologyMEDIUMvia Wikidata
Country	Saudi Arabia
Launch date	Jun 19, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	100HIGHvia 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/40016

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