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 62918U 26145.62166613 +.00000000 +00000-0 +12783-2 0 00001
2 62918 43.0009 243.7484 0001851 265.2412 94.8244 15.70829365 00
| Epoch (UTC): | 25 May 2026 14:55:11 |
| Eccentricity: | 0.0001851 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 243.7484° |
| argument of perigee: | 265.2412° |
| revolutions per day: | 15.70829365 |
| mean anomaly at epoch: | 94.8244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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