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 60239U 26152.55676365 +.00000000 +00000-0 +14397-3 0 00009
2 60239 62.0134 285.7563 0045419 133.2528 227.2368 15.00374430 08
| Epoch (UTC): | 01 June 2026 13:21:44 |
| Eccentricity: | 0.0045419 |
| inclination: | 62.0134° |
| perigee height: | 534 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 285.7563° |
| argument of perigee: | 133.2528° |
| revolutions per day: | 15.00374430 |
| mean anomaly at epoch: | 227.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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