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 54103U 26145.50024440 +.00000000 +00000-0 -25088-5 0 00002
2 54103 53.2136 329.0893 0001271 87.1263 272.9875 15.08837555 04
| Epoch (UTC): | 25 May 2026 12:00:21 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.0893° |
| argument of perigee: | 87.1263° |
| revolutions per day: | 15.08837555 |
| mean anomaly at epoch: | 272.9875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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