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 63022U 26145.37757556 +.00000000 +00000-0 +58844-3 0 00001
2 63022 42.9985 263.3763 0000660 40.0855 320.0045 15.27596971 02
| Epoch (UTC): | 25 May 2026 09:03:42 |
| Eccentricity: | 0.0000660 |
| inclination: | 42.9985° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 263.3763° |
| argument of perigee: | 40.0855° |
| revolutions per day: | 15.27596971 |
| mean anomaly at epoch: | 320.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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