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 65243U 26145.36953656 +.00000000 +00000-0 +28457-3 0 00003
2 65243 97.4454 188.1322 0002428 154.7378 205.3969 15.05657848 04
| Epoch (UTC): | 25 May 2026 08:52:07 |
| Eccentricity: | 0.0002428 |
| inclination: | 97.4454° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.1322° |
| argument of perigee: | 154.7378° |
| revolutions per day: | 15.05657848 |
| mean anomaly at epoch: | 205.3969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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