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 63035U 26145.32782575 +.00000000 +00000-0 +67947-3 0 00003
2 63035 53.1595 261.9225 0001028 101.5602 258.5516 15.34367311 06
| Epoch (UTC): | 25 May 2026 07:52:04 |
| Eccentricity: | 0.0001028 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.9225° |
| argument of perigee: | 101.5602° |
| revolutions per day: | 15.34367311 |
| mean anomaly at epoch: | 258.5516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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