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 65280U 26145.12781067 +.00000000 +00000-0 +26198-3 0 00003
2 65280 97.4480 197.6558 0002751 122.0977 238.0518 15.05659326 08
| Epoch (UTC): | 25 May 2026 03:04:02 |
| Eccentricity: | 0.0002751 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.6558° |
| argument of perigee: | 122.0977° |
| revolutions per day: | 15.05659326 |
| mean anomaly at epoch: | 238.0518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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