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 56773U 26145.33992331 +.00000000 +00000-0 +23273-4 0 00003
2 56773 69.9994 111.3660 0003673 266.4440 93.6299 14.98333954 06
| Epoch (UTC): | 25 May 2026 08:09:29 |
| Eccentricity: | 0.0003673 |
| inclination: | 69.9994° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 111.3660° |
| argument of perigee: | 266.4440° |
| revolutions per day: | 14.98333954 |
| mean anomaly at epoch: | 93.6299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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