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 60269U 26145.44124244 +.00000000 +00000-0 +22022-4 0 00001
2 60269 53.1614 55.6399 0001191 87.9391 272.1747 15.31703535 04
| Epoch (UTC): | 25 May 2026 10:35:23 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.6399° |
| argument of perigee: | 87.9391° |
| revolutions per day: | 15.31703535 |
| mean anomaly at epoch: | 272.1747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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