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 60362U 26145.43794978 +.00000000 +00000-0 +47674-4 0 00001
2 60362 53.1613 313.4237 0001493 79.8975 280.2194 15.30195499 05
| Epoch (UTC): | 25 May 2026 10:30:38 |
| Eccentricity: | 0.0001493 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.4237° |
| argument of perigee: | 79.8975° |
| revolutions per day: | 15.30195499 |
| mean anomaly at epoch: | 280.2194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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