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 54835U 26145.47556459 +.00000000 +00000-0 +57934-6 0 00005
2 54835 43.0029 62.6863 0000803 259.8095 100.2666 15.27574480 09
| Epoch (UTC): | 25 May 2026 11:24:48 |
| Eccentricity: | 0.0000803 |
| inclination: | 43.0029° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.6863° |
| argument of perigee: | 259.8095° |
| revolutions per day: | 15.27574480 |
| mean anomaly at epoch: | 100.2666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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