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 24279U 26099.83254030 +.00000000 +00000-0 +10183-3 0 00004
2 24279 98.7537 46.2341 0299456 358.6747 52.8868 13.47477955 09
| Epoch (UTC): | 09 April 2026 19:58:51 |
| Eccentricity: | 0.0299456 |
| inclination: | 98.7537° |
| perigee height: | 858 km |
| apogee height: | 1305 km |
| right ascension of ascending node: | 46.2341° |
| argument of perigee: | 358.6747° |
| revolutions per day: | 13.47477955 |
| mean anomaly at epoch: | 52.8868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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