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 62907U 26145.32498330 +.00000000 +00000-0 +22399-2 0 00004
2 62907 42.9999 245.8421 0001717 261.5270 98.5403 15.70943516 03
| Epoch (UTC): | 25 May 2026 07:47:58 |
| Eccentricity: | 0.0001717 |
| inclination: | 42.9999° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 245.8421° |
| argument of perigee: | 261.5270° |
| revolutions per day: | 15.70943516 |
| mean anomaly at epoch: | 98.5403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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