View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 51144U 26145.47868740 +.00000000 +00000-0 -34049-4 0 00005
2 51144 53.2154 314.4092 0001358 93.4920 266.6228 15.08837266 02
| Epoch (UTC): | 25 May 2026 11:29:18 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.4092° |
| argument of perigee: | 93.4920° |
| revolutions per day: | 15.08837266 |
| mean anomaly at epoch: | 266.6228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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