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 60024U 26145.23645911 +.00000000 +00000-0 +31135-4 0 00001
2 60024 53.1605 80.0395 0001222 87.7550 272.3590 15.30202730 09
| Epoch (UTC): | 25 May 2026 05:40:30 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.0395° |
| argument of perigee: | 87.7550° |
| revolutions per day: | 15.30202730 |
| mean anomaly at epoch: | 272.3590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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