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 62034U 26145.57985185 +.00000000 +00000-0 +22363-3 0 00003
2 62034 43.0003 182.2037 0001472 269.0481 91.0202 15.27585910 01
| Epoch (UTC): | 25 May 2026 13:54:59 |
| Eccentricity: | 0.0001472 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.2037° |
| argument of perigee: | 269.0481° |
| revolutions per day: | 15.27585910 |
| mean anomaly at epoch: | 91.0202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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