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 63702U 26145.50975976 +.00000000 +00000-0 +60751-3 0 00009
2 63702 53.1583 222.5584 0001684 91.4747 268.6448 15.31715141 01
| Epoch (UTC): | 25 May 2026 12:14:03 |
| Eccentricity: | 0.0001684 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 222.5584° |
| argument of perigee: | 91.4747° |
| revolutions per day: | 15.31715141 |
| mean anomaly at epoch: | 268.6448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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