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 53613U 26145.00348537 +.00000000 +00000-0 +70493-4 0 00006
2 53613 53.2145 251.6865 0001071 93.3018 266.8096 15.08839854 04
| Epoch (UTC): | 25 May 2026 00:05:01 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 251.6865° |
| argument of perigee: | 93.3018° |
| revolutions per day: | 15.08839854 |
| mean anomaly at epoch: | 266.8096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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