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 62306U 26145.42754875 +.00000000 +00000-0 +18338-3 0 00006
2 62306 53.1580 197.4215 0001104 82.1304 277.9822 15.30197356 01
| Epoch (UTC): | 25 May 2026 10:15:40 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.4215° |
| argument of perigee: | 82.1304° |
| revolutions per day: | 15.30197356 |
| mean anomaly at epoch: | 277.9822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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