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 26067.51186641 +.00000000 +00000-0 +56555-3 0 00003
2 60237 61.9903 209.2642 0051501 113.8913 246.7587 15.05777592 08
| Epoch (UTC): | 08 March 2026 12:17:05 |
| Eccentricity: | 0.0051501 |
| inclination: | 61.9903° |
| perigee height: | 513 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 209.2642° |
| argument of perigee: | 113.8913° |
| revolutions per day: | 15.05777592 |
| mean anomaly at epoch: | 246.7587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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