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 63604U 26145.62709325 +.00000000 +00000-0 +69060-4 0 00009
2 63604 99.6903 153.1799 0001235 93.4553 266.6727 13.57239359 05
| Epoch (UTC): | 25 May 2026 15:03:00 |
| Eccentricity: | 0.0001235 |
| inclination: | 99.6903° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.1799° |
| argument of perigee: | 93.4553° |
| revolutions per day: | 13.57239359 |
| mean anomaly at epoch: | 266.6727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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