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 55772U 26145.38087234 +.00000000 +00000-0 +43090-4 0 00002
2 55772 70.0001 30.9760 0002791 268.9259 91.1580 14.98331001 05
| Epoch (UTC): | 25 May 2026 09:08:27 |
| Eccentricity: | 0.0002791 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 30.9760° |
| argument of perigee: | 268.9259° |
| revolutions per day: | 14.98331001 |
| mean anomaly at epoch: | 91.1580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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