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 65237U 26145.57445214 +.00000000 +00000-0 +30447-3 0 00007
2 65237 97.4487 188.3181 0002262 118.5496 241.5959 15.05657458 01
| Epoch (UTC): | 25 May 2026 13:47:12 |
| Eccentricity: | 0.0002262 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3181° |
| argument of perigee: | 118.5496° |
| revolutions per day: | 15.05657458 |
| mean anomaly at epoch: | 241.5959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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