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 53487U 26145.34854316 +.00000000 +00000-0 +16354-3 0 00004
2 53487 97.4457 266.3984 0001369 138.8260 221.3070 15.05663732 03
| Epoch (UTC): | 25 May 2026 08:21:54 |
| Eccentricity: | 0.0001369 |
| inclination: | 97.4457° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.3984° |
| argument of perigee: | 138.8260° |
| revolutions per day: | 15.05663732 |
| mean anomaly at epoch: | 221.3070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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