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 24920U 26087.81744977 +.00000000 +00000-0 +10335-3 0 00005
2 24920 69.9537 195.5475 0020692 20.9240 339.2725 14.27909222 09
| Epoch (UTC): | 28 March 2026 19:37:07 |
| Eccentricity: | 0.0020692 |
| inclination: | 69.9537° |
| perigee height: | 784 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 195.5475° |
| argument of perigee: | 20.9240° |
| revolutions per day: | 14.27909222 |
| mean anomaly at epoch: | 339.2725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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