SAUDICOMSAT 2 is a payload in SSO orbit, operated by King Abdul Aziz City for Science and Technology, launched 2004.
| Orbit class | SSO |
| Inclination | 98.6639° |
| Eccentricity | 0.0055064 |
| Period | 99.3 min |
| Apogee | 765 km |
| Perigee | 687 km |
| Mean motion | 14.49991534 rev/day |
| RAAN | 200.8053° |
| Arg of perigee | 198.5745° |
| Mean anomaly | 161.3439° |
| B* | 5.8288e-5 |
| Rev at epoch | 16,297 |
1 28370U 04025E 26187.99897851 .00000180 00000-0 58288-4 0 99952 28370 98.6639 200.8053 0055064 198.5745 161.3439 14.49991534162971{
"OBJECT_NAME": "SAUDICOMSAT 2",
"OBJECT_ID": "2004-025E",
"EPOCH": "2026-07-06T23:58:31.743+00:00",
"MEAN_MOTION": 14.49991534,
"ECCENTRICITY": 0.0055064,
"INCLINATION": 98.6639,
"RA_OF_ASC_NODE": 200.8053,
"ARG_OF_PERICENTER": 198.5745,
"MEAN_ANOMALY": 161.3439,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 28370,
"REV_AT_EPOCH": 16297,
"BSTAR": 0.000058288,
"MEAN_MOTION_DOT": 0.0000018,
"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 | SAUDICOMSAT 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 |