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 26159.13957009 +.00000000 +00000-0 +57560-4 0 00009
2 24277 98.8002 213.4293 0002243 116.5661 243.5751 14.30395190 04
| Epoch (UTC): | 08 June 2026 03:20:58 |
| Eccentricity: | 0.0002243 |
| inclination: | 98.8002° |
| perigee height: | 789 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 213.4293° |
| argument of perigee: | 116.5661° |
| revolutions per day: | 14.30395190 |
| mean anomaly at epoch: | 243.5751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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