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 63854U 26145.03154219 +.00000000 +00000-0 +92107-3 0 00004
2 63854 43.0006 7.0920 0001888 261.5244 98.5394 15.27594121 03
| Epoch (UTC): | 25 May 2026 00:45:25 |
| Eccentricity: | 0.0001888 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.0920° |
| argument of perigee: | 261.5244° |
| revolutions per day: | 15.27594121 |
| mean anomaly at epoch: | 98.5394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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