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 26041.48110669 +.00000000 +00000-0 +91423-4 0 00007
2 24971 98.8361 32.7595 0051112 240.4307 119.1778 14.35455637 08
| Epoch (UTC): | 10 February 2026 11:32:47 |
| Eccentricity: | 0.0051112 |
| inclination: | 98.8361° |
| perigee height: | 737 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 32.7595° |
| argument of perigee: | 240.4307° |
| revolutions per day: | 14.35455637 |
| mean anomaly at epoch: | 119.1778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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