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 52789U 26145.57378809 +.00000000 +00000-0 +34129-3 0 00001
2 52789 49.9869 288.3083 0001383 284.9734 75.1059 15.00451496 04
| Epoch (UTC): | 25 May 2026 13:46:15 |
| Eccentricity: | 0.0001383 |
| inclination: | 49.9869° |
| perigee height: | 565 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 288.3083° |
| argument of perigee: | 284.9734° |
| revolutions per day: | 15.00451496 |
| mean anomaly at epoch: | 75.1059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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