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 54853U 26145.45809095 +.00000000 +00000-0 -13184-4 0 00008
2 54853 43.0072 47.8399 0001475 246.7561 113.3136 15.27568770 07
| Epoch (UTC): | 25 May 2026 10:59:39 |
| Eccentricity: | 0.0001475 |
| inclination: | 43.0072° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 47.8399° |
| argument of perigee: | 246.7561° |
| revolutions per day: | 15.27568770 |
| mean anomaly at epoch: | 113.3136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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