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 45544U 26144.97657891 +.00000000 +00000-0 +44372-3 0 00007
2 45544 53.0453 77.8195 0004064 41.4434 318.6889 15.67992149 01
| Epoch (UTC): | 24 May 2026 23:26:16 |
| Eccentricity: | 0.0004064 |
| inclination: | 53.0453° |
| perigee height: | 362 km |
| apogee height: | 367 km |
| right ascension of ascending node: | 77.8195° |
| argument of perigee: | 41.4434° |
| revolutions per day: | 15.67992149 |
| mean anomaly at epoch: | 318.6889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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