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 60036U 26145.51038059 +.00000000 +00000-0 -13852-3 0 00000
2 60036 53.1607 78.8988 0001011 81.0386 279.0729 15.30217018 00
| Epoch (UTC): | 25 May 2026 12:14:56 |
| Eccentricity: | 0.0001011 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.8988° |
| argument of perigee: | 81.0386° |
| revolutions per day: | 15.30217018 |
| mean anomaly at epoch: | 279.0729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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