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 24920U 26040.18232692 +.00000000 +00000-0 +12296-3 0 00008
2 24920 69.9541 303.1354 0018989 93.8239 266.5054 14.27882834 06
| Epoch (UTC): | 09 February 2026 04:22:33 |
| Eccentricity: | 0.0018989 |
| inclination: | 69.9541° |
| perigee height: | 785 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 303.1354° |
| argument of perigee: | 93.8239° |
| revolutions per day: | 14.27882834 |
| mean anomaly at epoch: | 266.5054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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