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 63294U 26145.59007206 +.00000000 +00000-0 +43325-3 0 00004
2 63294 97.6489 285.1922 0014732 212.3880 147.6450 15.16226701 07
| Epoch (UTC): | 25 May 2026 14:09:42 |
| Eccentricity: | 0.0014732 |
| inclination: | 97.6489° |
| perigee height: | 507 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 285.1922° |
| argument of perigee: | 212.3880° |
| revolutions per day: | 15.16226701 |
| mean anomaly at epoch: | 147.6450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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