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 26121.88902436 +.00000000 +00000-0 +29795-3 0 00008
2 60237 61.9921 18.6562 0046473 124.9299 235.6173 15.06261997 09
| Epoch (UTC): | 01 May 2026 21:20:11 |
| Eccentricity: | 0.0046473 |
| inclination: | 61.9921° |
| perigee height: | 515 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 18.6562° |
| argument of perigee: | 124.9299° |
| revolutions per day: | 15.06261997 |
| mean anomaly at epoch: | 235.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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