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 60043U 26144.73161110 +.00000000 +00000-0 +44130-4 0 00009
2 60043 53.1581 251.4526 0000792 88.1984 271.9124 15.69740459 05
| Epoch (UTC): | 24 May 2026 17:33:31 |
| Eccentricity: | 0.0000792 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 251.4526° |
| argument of perigee: | 88.1984° |
| revolutions per day: | 15.69740459 |
| mean anomaly at epoch: | 271.9124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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