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 00051U 26103.07675353 +.00000000 +00000-0 -62235-3 0 00009
2 00051 47.2124 250.8319 0107308 3.6986 356.4575 12.18377831 03
| Epoch (UTC): | 13 April 2026 01:50:31 |
| Eccentricity: | 0.0107308 |
| inclination: | 47.2124° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 250.8319° |
| argument of perigee: | 3.6986° |
| revolutions per day: | 12.18377831 |
| mean anomaly at epoch: | 356.4575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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