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 26158.52283230 +.00000000 +00000-0 +41172-3 0 00004
2 00051 47.2126 79.2580 0106491 168.0567 192.2780 12.18377803 04
| Epoch (UTC): | 07 June 2026 12:32:52 |
| Eccentricity: | 0.0106491 |
| inclination: | 47.2126° |
| perigee height: | 1515 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 79.2580° |
| argument of perigee: | 168.0567° |
| revolutions per day: | 12.18377803 |
| mean anomaly at epoch: | 192.2780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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