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 65295U 26145.10564818 +.00000000 +00000-0 +16326-3 0 00002
2 65295 97.4506 197.5320 0001674 134.4257 225.7108 15.05656462 06
| Epoch (UTC): | 25 May 2026 02:32:08 |
| Eccentricity: | 0.0001674 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.5320° |
| argument of perigee: | 134.4257° |
| revolutions per day: | 15.05656462 |
| mean anomaly at epoch: | 225.7108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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