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 51972U 26145.41616051 +.00000000 +00000-0 +11200-5 0 00008
2 51972 53.1566 40.2310 0001375 91.1539 268.9619 15.29354401 01
| Epoch (UTC): | 25 May 2026 09:59:16 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.1566° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 40.2310° |
| argument of perigee: | 91.1539° |
| revolutions per day: | 15.29354401 |
| mean anomaly at epoch: | 268.9619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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