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 60345U 26145.54406289 +.00000000 +00000-0 +29615-4 0 00004
2 60345 53.1612 78.5139 0001392 92.7688 267.3472 15.30189732 06
| Epoch (UTC): | 25 May 2026 13:03:27 |
| Eccentricity: | 0.0001392 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.5139° |
| argument of perigee: | 92.7688° |
| revolutions per day: | 15.30189732 |
| mean anomaly at epoch: | 267.3472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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