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 55971U 26145.55703498 +.00000000 +00000-0 +00000-0 0 00009
2 55971 0.0189 299.6506 0001650 119.7945 249.3262 1.00271350 09
| Epoch (UTC): | 25 May 2026 13:22:07 |
| Eccentricity: | 0.0001650 |
| inclination: | 0.0189° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 299.6506° |
| argument of perigee: | 119.7945° |
| revolutions per day: | 1.00271350 |
| mean anomaly at epoch: | 249.3262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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