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 26064.55314701 +.00000000 +00000-0 +10631-3 0 00004
2 24971 98.8392 56.3884 0052250 171.8919 188.3122 14.35467787 05
| Epoch (UTC): | 05 March 2026 13:16:31 |
| Eccentricity: | 0.0052250 |
| inclination: | 98.8392° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 56.3884° |
| argument of perigee: | 171.8919° |
| revolutions per day: | 14.35467787 |
| mean anomaly at epoch: | 188.3122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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