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 62314U 26145.36012316 +.00000000 +00000-0 +26175-3 0 00003
2 62314 53.1580 197.7103 0000869 69.8937 290.2157 15.30198676 05
| Epoch (UTC): | 25 May 2026 08:38:34 |
| Eccentricity: | 0.0000869 |
| inclination: | 53.1580° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.7103° |
| argument of perigee: | 69.8937° |
| revolutions per day: | 15.30198676 |
| mean anomaly at epoch: | 290.2157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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