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 52608U 26145.15204620 +.00000000 +00000-0 +57109-4 0 00008
2 52608 53.2147 295.8682 0001358 90.4434 269.6714 15.08840742 00
| Epoch (UTC): | 25 May 2026 03:38:56 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 295.8682° |
| argument of perigee: | 90.4434° |
| revolutions per day: | 15.08840742 |
| mean anomaly at epoch: | 269.6714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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