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 45780U 26145.46056205 +.00000000 +00000-0 +96042-3 0 00007
2 45780 53.0454 166.8044 0007884 31.4968 328.6515 15.60512652 07
| Epoch (UTC): | 25 May 2026 11:03:12 |
| Eccentricity: | 0.0007884 |
| inclination: | 53.0454° |
| perigee height: | 381 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 166.8044° |
| argument of perigee: | 31.4968° |
| revolutions per day: | 15.60512652 |
| mean anomaly at epoch: | 328.6515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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