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 24971U 26087.90377942 +.00000000 +00000-0 +92342-4 0 00004
2 24971 98.8412 80.3114 0053182 104.0187 256.6918 14.35480187 02
| Epoch (UTC): | 28 March 2026 21:41:26 |
| Eccentricity: | 0.0053182 |
| inclination: | 98.8412° |
| perigee height: | 735 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 80.3114° |
| argument of perigee: | 104.0187° |
| revolutions per day: | 14.35480187 |
| mean anomaly at epoch: | 256.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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