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 24277U 26053.65318127 +.00000000 +00000-0 +50491-4 0 00007
2 24277 98.8171 106.6400 0002320 90.9064 269.2383 14.30363050 08
| Epoch (UTC): | 22 February 2026 15:40:34 |
| Eccentricity: | 0.0002320 |
| inclination: | 98.8171° |
| perigee height: | 789 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 106.6400° |
| argument of perigee: | 90.9064° |
| revolutions per day: | 14.30363050 |
| mean anomaly at epoch: | 269.2383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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