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 53508U 26145.57838976 +.00000000 +00000-0 -15733-3 0 00008
2 53508 97.4446 266.6423 0001982 138.3409 221.7969 15.05644206 03
| Epoch (UTC): | 25 May 2026 13:52:52 |
| Eccentricity: | 0.0001982 |
| inclination: | 97.4446° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.6423° |
| argument of perigee: | 138.3409° |
| revolutions per day: | 15.05644206 |
| mean anomaly at epoch: | 221.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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