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 24796U 26087.96856925 +.00000000 +00000-0 +14629-3 0 00009
2 24796 86.3938 54.1878 0002105 85.7144 274.4294 14.37109180 03
| Epoch (UTC): | 28 March 2026 23:14:44 |
| Eccentricity: | 0.0002105 |
| inclination: | 86.3938° |
| perigee height: | 767 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 54.1878° |
| argument of perigee: | 85.7144° |
| revolutions per day: | 14.37109180 |
| mean anomaly at epoch: | 274.4294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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