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 60453U 26145.59736601 +.00000000 +00000-0 +21997-3 0 00007
2 60453 45.0009 243.6026 0013134 188.4629 171.6029 15.15846462 09
| Epoch (UTC): | 25 May 2026 14:20:12 |
| Eccentricity: | 0.0013134 |
| inclination: | 45.0009° |
| perigee height: | 509 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 243.6026° |
| argument of perigee: | 188.4629° |
| revolutions per day: | 15.15846462 |
| mean anomaly at epoch: | 171.6029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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