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 24827U 26129.79498676 +.00000000 +00000-0 -83880-3 0 00003
2 24827 63.3059 270.2496 1090458 69.2451 32.0016 11.07978614 01
| Epoch (UTC): | 09 May 2026 19:04:46 |
| Eccentricity: | 0.1090458 |
| inclination: | 63.3059° |
| perigee height: | 1194 km |
| apogee height: | 3048 km |
| right ascension of ascending node: | 270.2496° |
| argument of perigee: | 69.2451° |
| revolutions per day: | 11.07978614 |
| mean anomaly at epoch: | 32.0016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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