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 53164U 26145.47358759 +.00000000 +00000-0 +19257-4 0 00006
2 53164 53.2106 179.4255 0000843 77.0345 283.0741 15.08840517 06
| Epoch (UTC): | 25 May 2026 11:21:57 |
| Eccentricity: | 0.0000843 |
| inclination: | 53.2106° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 179.4255° |
| argument of perigee: | 77.0345° |
| revolutions per day: | 15.08840517 |
| mean anomaly at epoch: | 283.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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