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 63202U 26145.35630303 +.00000000 +00000-0 +41076-3 0 00008
2 63202 42.9994 12.6636 0000611 142.8136 217.2758 15.27592379 01
| Epoch (UTC): | 25 May 2026 08:33:04 |
| Eccentricity: | 0.0000611 |
| inclination: | 42.9994° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 12.6636° |
| argument of perigee: | 142.8136° |
| revolutions per day: | 15.27592379 |
| mean anomaly at epoch: | 217.2758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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