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 65380U 26145.39644264 +.00000000 +00000-0 +32652-3 0 00002
2 65380 97.4531 16.7838 0001937 79.4711 280.6734 15.05660566 05
| Epoch (UTC): | 25 May 2026 09:30:52 |
| Eccentricity: | 0.0001937 |
| inclination: | 97.4531° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.7838° |
| argument of perigee: | 79.4711° |
| revolutions per day: | 15.05660566 |
| mean anomaly at epoch: | 280.6734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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