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 26161.63653578 +.00000000 +00000-0 +60629-4 0 00003
2 24279 98.7588 100.4632 0298849 200.7031 340.0152 13.47482163 04
| Epoch (UTC): | 10 June 2026 15:16:36 |
| Eccentricity: | 0.0298849 |
| inclination: | 98.7588° |
| perigee height: | 859 km |
| apogee height: | 1304 km |
| right ascension of ascending node: | 100.4632° |
| argument of perigee: | 200.7031° |
| revolutions per day: | 13.47482163 |
| mean anomaly at epoch: | 340.0152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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