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 62012U 26145.65115295 +.00000000 +00000-0 +20636-2 0 00005
2 62012 53.1577 21.8117 0000466 169.2563 190.8465 15.69874040 06
| Epoch (UTC): | 25 May 2026 15:37:39 |
| Eccentricity: | 0.0000466 |
| inclination: | 53.1577° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 21.8117° |
| argument of perigee: | 169.2563° |
| revolutions per day: | 15.69874040 |
| mean anomaly at epoch: | 190.8465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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