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 60414U 26145.57148181 +.00000000 +00000-0 +35257-4 0 00007
2 60414 53.1579 245.3322 0001522 85.9004 274.2172 15.31692502 03
| Epoch (UTC): | 25 May 2026 13:42:56 |
| Eccentricity: | 0.0001522 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.3322° |
| argument of perigee: | 85.9004° |
| revolutions per day: | 15.31692502 |
| mean anomaly at epoch: | 274.2172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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