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 52612U 26144.68468808 +.00000000 +00000-0 +17170-4 0 00004
2 52612 53.2147 297.9662 0001403 87.6394 272.4758 15.08839761 09
| Epoch (UTC): | 24 May 2026 16:25:57 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 297.9662° |
| argument of perigee: | 87.6394° |
| revolutions per day: | 15.08839761 |
| mean anomaly at epoch: | 272.4758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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