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 24773U 26159.10119677 +.00000000 +00000-0 +39941-4 0 00001
2 24773 82.9206 103.4017 0024101 180.0889 190.8612 13.73977438 09
| Epoch (UTC): | 08 June 2026 02:25:43 |
| Eccentricity: | 0.0024101 |
| inclination: | 82.9206° |
| perigee height: | 968 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 103.4017° |
| argument of perigee: | 180.0889° |
| revolutions per day: | 13.73977438 |
| mean anomaly at epoch: | 190.8612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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