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 60063U 26145.35483174 +.00000000 +00000-0 -62960-5 0 00000
2 60063 53.1583 173.1834 0000904 76.6316 283.4803 15.69713466 07
| Epoch (UTC): | 25 May 2026 08:30:57 |
| Eccentricity: | 0.0000904 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.1834° |
| argument of perigee: | 76.6316° |
| revolutions per day: | 15.69713466 |
| mean anomaly at epoch: | 283.4803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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