SAUDISAT 2 is a payload in SSO orbit, operated by King Abdul Aziz City for Science and Technology, launched 2004.
| Orbit class | SSO |
| Inclination | 98.5514° |
| Eccentricity | 0.0023655 |
| Period | 98.9 min |
| Apogee | 721 km |
| Perigee | 687 km |
| Mean motion | 14.56695117 rev/day |
| RAAN | 188.4419° |
| Arg of perigee | 234.4243° |
| Mean anomaly | 125.4749° |
| B* | 5.8559e-5 |
| Rev at epoch | 16,862 |
1 28371U 04025F 26187.94878641 .00000213 00000-0 58559-4 0 99952 28371 98.5514 188.4419 0023655 234.4243 125.4749 14.56695117168623{
"OBJECT_NAME": "SAUDISAT 2",
"OBJECT_ID": "2004-025F",
"EPOCH": "2026-07-06T22:46:15.146+00:00",
"MEAN_MOTION": 14.56695117,
"ECCENTRICITY": 0.0023655,
"INCLINATION": 98.5514,
"RA_OF_ASC_NODE": 188.4419,
"ARG_OF_PERICENTER": 234.4243,
"MEAN_ANOMALY": 125.4749,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 28371,
"REV_AT_EPOCH": 16862,
"BSTAR": 0.000058559,
"MEAN_MOTION_DOT": 0.00000213,
"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.
| Name | SAUDISAT 2 |
| Operator | |
| Country | Saudi Arabia |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |