▸Orbital parameters

Orbit class	SSO
Inclination	98.3155°
Eccentricity	0.0038877
Period	97.9 min
Apogee	686 km
Perigee	631 km
Mean motion	14.70740625 rev/day
RAAN	163.7394°
Arg of perigee	351.7392°
Mean anomaly	8.3169°
B*	1.3340e-4
Rev at epoch	2,772

▸Two-line element set (TLE)

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

1 31125U 07012J 26187.91304544 .00000768 00000-0 13340-3 0 9991

2 31125 98.3155 163.7394 0038877 351.7392 8.3169 14.70740625 27722

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SAUDICOMSAT 3",
  "OBJECT_ID": "2007-012J",
  "EPOCH": "2026-07-06T21:54:47.126+00:00",
  "MEAN_MOTION": 14.70740625,
  "ECCENTRICITY": 0.0038877,
  "INCLINATION": 98.3155,
  "RA_OF_ASC_NODE": 163.7394,
  "ARG_OF_PERICENTER": 351.7392,
  "MEAN_ANOMALY": 8.3169,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 31125,
  "REV_AT_EPOCH": 2772,
  "BSTAR": 0.0001334,
  "MEAN_MOTION_DOT": 0.00000768,
  "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	SAUDICOMSAT 3
Operator	King Abdul Aziz City for Science and TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Saudi Arabia
Launch date	Apr 17, 2007HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/31125

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