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 65390U 26145.23859704 +.00000000 +00000-0 +34522-3 0 00001
2 65390 97.4479 16.5355 0002455 79.5738 280.5765 15.05661120 05
| Epoch (UTC): | 25 May 2026 05:43:34 |
| Eccentricity: | 0.0002455 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.5355° |
| argument of perigee: | 79.5738° |
| revolutions per day: | 15.05661120 |
| mean anomaly at epoch: | 280.5765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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