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 60237U 26145.38797984 +.00000000 +00000-0 +30387-3 0 00008
2 60237 61.9903 296.2458 0043830 129.9022 230.5937 15.06425335 00
| Epoch (UTC): | 25 May 2026 09:18:41 |
| Eccentricity: | 0.0043830 |
| inclination: | 61.9903° |
| perigee height: | 517 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 296.2458° |
| argument of perigee: | 129.9022° |
| revolutions per day: | 15.06425335 |
| mean anomaly at epoch: | 230.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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