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 65795U 26145.55368531 +.00000000 +00000-0 +17482-3 0 00004
2 65795 97.4476 8.3010 0002387 90.5013 269.6487 15.05654346 02
| Epoch (UTC): | 25 May 2026 13:17:18 |
| Eccentricity: | 0.0002387 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.3010° |
| argument of perigee: | 90.5013° |
| revolutions per day: | 15.05654346 |
| mean anomaly at epoch: | 269.6487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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