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 62795U 26145.55869684 +.00000000 +00000-0 +13904-3 0 00001
2 62795 88.9717 86.0411 0011918 224.6628 135.3564 13.51009102 00
| Epoch (UTC): | 25 May 2026 13:24:31 |
| Eccentricity: | 0.0011918 |
| inclination: | 88.9717° |
| perigee height: | 1060 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 86.0411° |
| argument of perigee: | 224.6628° |
| revolutions per day: | 13.51009102 |
| mean anomaly at epoch: | 135.3564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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