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 60412U 26144.99677863 +.00000000 +00000-0 +23125-4 0 00005
2 60412 53.1620 247.4363 0001098 102.7025 257.4101 15.34387522 06
| Epoch (UTC): | 24 May 2026 23:55:21 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1620° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.4363° |
| argument of perigee: | 102.7025° |
| revolutions per day: | 15.34387522 |
| mean anomaly at epoch: | 257.4101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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