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 59072U 26145.60338823 +.00000000 +00000-0 +66358-4 0 00009
2 59072 88.9807 286.5697 0018587 57.8412 302.4593 14.45998908 07
| Epoch (UTC): | 25 May 2026 14:28:52 |
| Eccentricity: | 0.0018587 |
| inclination: | 88.9807° |
| perigee height: | 726 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 286.5697° |
| argument of perigee: | 57.8412° |
| revolutions per day: | 14.45998908 |
| mean anomaly at epoch: | 302.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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