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 53985U 26145.49109641 +.00000000 +00000-0 +75745-5 0 00008
2 53985 53.2135 229.5801 0001032 80.2547 279.8562 15.08839678 04
| Epoch (UTC): | 25 May 2026 11:47:10 |
| Eccentricity: | 0.0001032 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 229.5801° |
| argument of perigee: | 80.2547° |
| revolutions per day: | 15.08839678 |
| mean anomaly at epoch: | 279.8562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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