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 60316U 26145.42046875 +.00000000 +00000-0 +38327-4 0 00000
2 60316 53.1600 300.2653 0001269 94.4607 265.6539 15.30191674 03
| Epoch (UTC): | 25 May 2026 10:05:28 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.2653° |
| argument of perigee: | 94.4607° |
| revolutions per day: | 15.30191674 |
| mean anomaly at epoch: | 265.6539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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