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 65297U 26145.27960464 +.00000000 +00000-0 +11073-2 0 00002
2 65297 97.9620 228.8210 0016848 154.0045 206.2016 14.78855682 04
| Epoch (UTC): | 25 May 2026 06:42:37 |
| Eccentricity: | 0.0016848 |
| inclination: | 97.9620° |
| perigee height: | 621 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 228.8210° |
| argument of perigee: | 154.0045° |
| revolutions per day: | 14.78855682 |
| mean anomaly at epoch: | 206.2016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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