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 63283U 26145.55465628 +.00000000 +00000-0 +36997-3 0 00001
2 63283 42.9993 167.2738 0001696 276.4185 83.6474 15.27580487 08
| Epoch (UTC): | 25 May 2026 13:18:42 |
| Eccentricity: | 0.0001696 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.2738° |
| argument of perigee: | 276.4185° |
| revolutions per day: | 15.27580487 |
| mean anomaly at epoch: | 83.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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