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 63316U 26145.36494700 +.00000000 +00000-0 +18434-2 0 00005
2 63316 43.0001 162.6242 0001486 250.4630 109.6077 15.70907457 06
| Epoch (UTC): | 25 May 2026 08:45:31 |
| Eccentricity: | 0.0001486 |
| inclination: | 43.0001° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.6242° |
| argument of perigee: | 250.4630° |
| revolutions per day: | 15.70907457 |
| mean anomaly at epoch: | 109.6077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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