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 60235U 26162.31244066 +.00000000 +00000-0 +15675-3 0 00009
2 60235 61.9942 251.6766 0051079 134.5130 226.0152 15.01125843 09
| Epoch (UTC): | 11 June 2026 07:29:54 |
| Eccentricity: | 0.0051079 |
| inclination: | 61.9942° |
| perigee height: | 528 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 251.6766° |
| argument of perigee: | 134.5130° |
| revolutions per day: | 15.01125843 |
| mean anomaly at epoch: | 226.0152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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