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 51971U 26145.38717370 +.00000000 +00000-0 -43827-4 0 00009
2 51971 53.1620 27.7664 0001661 90.6652 269.4540 15.31706760 02
| Epoch (UTC): | 25 May 2026 09:17:31 |
| Eccentricity: | 0.0001661 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 27.7664° |
| argument of perigee: | 90.6652° |
| revolutions per day: | 15.31706760 |
| mean anomaly at epoch: | 269.4540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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