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 63030U 26145.39095918 +.00000000 +00000-0 +45460-3 0 00009
2 63030 53.1580 275.1006 0001073 103.7141 256.3980 15.30211576 09
| Epoch (UTC): | 25 May 2026 09:22:58 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.1006° |
| argument of perigee: | 103.7141° |
| revolutions per day: | 15.30211576 |
| mean anomaly at epoch: | 256.3980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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