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 63055U 26145.35751565 +.00000000 +00000-0 +14539-2 0 00001
2 63055 43.0000 272.7739 0001976 256.5415 103.5233 15.70953560 04
| Epoch (UTC): | 25 May 2026 08:34:49 |
| Eccentricity: | 0.0001976 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 272.7739° |
| argument of perigee: | 256.5415° |
| revolutions per day: | 15.70953560 |
| mean anomaly at epoch: | 103.5233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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