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 60349U 26145.51303773 +.00000000 +00000-0 +37360-4 0 00005
2 60349 53.1609 77.6142 0001203 94.5568 265.5572 15.34392285 02
| Epoch (UTC): | 25 May 2026 12:18:46 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 77.6142° |
| argument of perigee: | 94.5568° |
| revolutions per day: | 15.34392285 |
| mean anomaly at epoch: | 265.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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