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 53143U 26145.41378627 +.00000000 +00000-0 -46246-4 0 00002
2 53143 53.2113 189.6920 0001948 95.2705 264.8509 15.08842133 07
| Epoch (UTC): | 25 May 2026 09:55:51 |
| Eccentricity: | 0.0001948 |
| inclination: | 53.2113° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.6920° |
| argument of perigee: | 95.2705° |
| revolutions per day: | 15.08842133 |
| mean anomaly at epoch: | 264.8509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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