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 28057U 26087.89317160 +.00000000 +00000-0 +88647-4 0 00000
2 28057 98.7481 58.4205 0001771 63.6996 296.4371 14.36710461 05
| Epoch (UTC): | 28 March 2026 21:26:10 |
| Eccentricity: | 0.0001771 |
| inclination: | 98.7481° |
| perigee height: | 768 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 58.4205° |
| argument of perigee: | 63.6996° |
| revolutions per day: | 14.36710461 |
| mean anomaly at epoch: | 296.4371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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