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 63408U 26145.11334242 +.00000000 +00000-0 +82258-3 0 00000
2 63408 43.0013 39.3005 0001656 263.0063 97.0600 15.27592162 04
| Epoch (UTC): | 25 May 2026 02:43:12 |
| Eccentricity: | 0.0001656 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.3005° |
| argument of perigee: | 263.0063° |
| revolutions per day: | 15.27592162 |
| mean anomaly at epoch: | 97.0600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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