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 45580U 26145.51093856 +.00000000 +00000-0 +82848-3 0 00003
2 45580 53.1552 80.3476 0003171 87.1533 272.9832 15.33822088 05
| Epoch (UTC): | 25 May 2026 12:15:45 |
| Eccentricity: | 0.0003171 |
| inclination: | 53.1552° |
| perigee height: | 462 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 80.3476° |
| argument of perigee: | 87.1533° |
| revolutions per day: | 15.33822088 |
| mean anomaly at epoch: | 272.9832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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