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 65802U 26145.40138631 +.00000000 +00000-0 +28089-3 0 00008
2 65802 97.4485 8.1988 0002063 81.7403 278.4058 15.05660522 04
| Epoch (UTC): | 25 May 2026 09:37:59 |
| Eccentricity: | 0.0002063 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1988° |
| argument of perigee: | 81.7403° |
| revolutions per day: | 15.05660522 |
| mean anomaly at epoch: | 278.4058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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