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 53489U 26145.57979013 +.00000000 +00000-0 -48084-4 0 00000
2 53489 97.4458 265.4736 0001069 159.0807 201.0464 15.05649996 08
| Epoch (UTC): | 25 May 2026 13:54:53 |
| Eccentricity: | 0.0001069 |
| inclination: | 97.4458° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.4736° |
| argument of perigee: | 159.0807° |
| revolutions per day: | 15.05649996 |
| mean anomaly at epoch: | 201.0464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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