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 37348U 11002A 24262.08462643 0.00057000 00000-0 53026-3 0 02
2 37348 97.8772 37.0228 0503871 200.0756 159.9242 14.84682940 01
| Epoch (UTC): | 18 September 2024 02:01:51 |
| Eccentricity: | 0.0503871 |
| inclination: | 97.8772° |
| perigee height: | 262 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 37.0228° |
| argument of perigee: | 200.0756° |
| revolutions per day: | 14.84682940 |
| mean anomaly at epoch: | 159.9242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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