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 26020.91833227 +.00000000 +00000-0 +17753-3 0 00007
2 24971 98.8333 11.7090 0051266 302.2176 57.4044 14.35439161 09
| Epoch (UTC): | 20 January 2026 22:02:23 |
| Eccentricity: | 0.0051266 |
| inclination: | 98.8333° |
| perigee height: | 737 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 11.7090° |
| argument of perigee: | 302.2176° |
| revolutions per day: | 14.35439161 |
| mean anomaly at epoch: | 57.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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