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 54165U 26145.36963032 +.00000000 +00000-0 +10990-4 0 00007
2 54165 53.2124 29.8645 0001366 82.7152 277.3995 15.08830014 07
| Epoch (UTC): | 25 May 2026 08:52:16 |
| Eccentricity: | 0.0001366 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.8645° |
| argument of perigee: | 82.7152° |
| revolutions per day: | 15.08830014 |
| mean anomaly at epoch: | 277.3995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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