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 26044.91820062 +.00000000 +00000-0 +21588-3 0 00000
2 60235 61.9949 299.8183 0062177 107.3366 253.4538 15.00472422 02
| Epoch (UTC): | 13 February 2026 22:02:12 |
| Eccentricity: | 0.0062177 |
| inclination: | 61.9949° |
| perigee height: | 522 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 299.8183° |
| argument of perigee: | 107.3366° |
| revolutions per day: | 15.00472422 |
| mean anomaly at epoch: | 253.4538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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