HELLAS-SAT 2 is a payload in GEO orbit, operated by HellasSat Consortium Ltd., OTE Group, launched 2003.
| Orbit class | GEO |
| Inclination | 7.4004° |
| Eccentricity | 0.0003312 |
| Period | 1436.1 min |
| Apogee | 35,801 km |
| Perigee | 35,773 km |
| Mean motion | 1.00271721 rev/day |
| RAAN | 67.6464° |
| Arg of perigee | 69.2487° |
| Mean anomaly | 112.4938° |
| B* | 0.0000e+0 |
| Rev at epoch | 4,304 |
1 27811U 03020A 26187.92919431 -.00000073 00000-0 00000-0 0 99972 27811 7.4004 67.6464 0003312 69.2487 112.4938 1.00271721 43044{
"OBJECT_NAME": "HELLAS-SAT 2",
"OBJECT_ID": "2003-020A",
"EPOCH": "2026-07-06T22:18:02.388+00:00",
"MEAN_MOTION": 1.00271721,
"ECCENTRICITY": 0.0003312,
"INCLINATION": 7.4004,
"RA_OF_ASC_NODE": 67.6464,
"ARG_OF_PERICENTER": 69.2487,
"MEAN_ANOMALY": 112.4938,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 27811,
"REV_AT_EPOCH": 4304,
"BSTAR": 0,
"MEAN_MOTION_DOT": -7.3e-7,
"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 | HELLAS-SAT 2 |
| Operator | |
| Country | Greece |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |