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 55770U 26145.40575464 +.00000000 +00000-0 -76548-5 0 00006
2 55770 70.0005 31.0616 0002399 268.7089 91.3795 14.98329114 04
| Epoch (UTC): | 25 May 2026 09:44:17 |
| Eccentricity: | 0.0002399 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.0616° |
| argument of perigee: | 268.7089° |
| revolutions per day: | 14.98329114 |
| mean anomaly at epoch: | 91.3795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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