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 26160.28837529 +.00000000 +00000-0 +67964-4 0 00002
2 24279 98.7588 99.2800 0298796 204.1488 280.1674 13.47482087 09
| Epoch (UTC): | 09 June 2026 06:55:15 |
| Eccentricity: | 0.0298796 |
| inclination: | 98.7588° |
| perigee height: | 859 km |
| apogee height: | 1304 km |
| right ascension of ascending node: | 99.2800° |
| argument of perigee: | 204.1488° |
| revolutions per day: | 13.47482087 |
| mean anomaly at epoch: | 280.1674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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