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 51985U 26145.44373182 +.00000000 +00000-0 +88704-4 0 00002
2 51985 53.2122 54.5671 0001276 85.5322 274.5816 15.08830708 07
| Epoch (UTC): | 25 May 2026 10:38:58 |
| Eccentricity: | 0.0001276 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 54.5671° |
| argument of perigee: | 85.5322° |
| revolutions per day: | 15.08830708 |
| mean anomaly at epoch: | 274.5816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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