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 63953U 26145.37440620 +.00000000 +00000-0 +82502-3 0 00003
2 63953 43.0001 103.1975 0001280 267.0614 93.0091 15.27606456 03
| Epoch (UTC): | 25 May 2026 08:59:08 |
| Eccentricity: | 0.0001280 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1975° |
| argument of perigee: | 267.0614° |
| revolutions per day: | 15.27606456 |
| mean anomaly at epoch: | 93.0091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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