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 53086U 26145.22120197 +.00000000 +00000-0 -96571-4 0 00000
2 53086 97.4474 325.2412 0001361 86.1170 274.0213 15.05656091 09
| Epoch (UTC): | 25 May 2026 05:18:31 |
| Eccentricity: | 0.0001361 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.2412° |
| argument of perigee: | 86.1170° |
| revolutions per day: | 15.05656091 |
| mean anomaly at epoch: | 274.0213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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