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 57628U 26145.63535449 +.00000000 +00000-0 +18464-3 0 00004
2 57628 44.9994 50.5074 0005147 155.5316 204.5787 14.62210865 01
| Epoch (UTC): | 25 May 2026 15:14:54 |
| Eccentricity: | 0.0005147 |
| inclination: | 44.9994° |
| perigee height: | 682 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 50.5074° |
| argument of perigee: | 155.5316° |
| revolutions per day: | 14.62210865 |
| mean anomaly at epoch: | 204.5787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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