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 60739U 26145.33871350 +.00000000 +00000-0 +30752-4 0 00007
2 60739 53.1612 272.5791 0001086 96.4828 263.6297 15.30190000 04
| Epoch (UTC): | 25 May 2026 08:07:44 |
| Eccentricity: | 0.0001086 |
| inclination: | 53.1612° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 272.5791° |
| argument of perigee: | 96.4828° |
| revolutions per day: | 15.30190000 |
| mean anomaly at epoch: | 263.6297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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