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 62985U 26145.31742493 +.00000000 +00000-0 +12504-2 0 00008
2 62985 42.9989 259.5999 0001881 268.4035 91.6617 15.70934657 04
| Epoch (UTC): | 25 May 2026 07:37:05 |
| Eccentricity: | 0.0001881 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 259.5999° |
| argument of perigee: | 268.4035° |
| revolutions per day: | 15.70934657 |
| mean anomaly at epoch: | 91.6617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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