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 63918U 26145.61130252 +.00000000 +00000-0 +32943-4 0 00003
2 63918 85.9969 198.0811 0002470 104.8812 255.2644 14.12442974 06
| Epoch (UTC): | 25 May 2026 14:40:16 |
| Eccentricity: | 0.0002470 |
| inclination: | 85.9969° |
| perigee height: | 849 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 198.0811° |
| argument of perigee: | 104.8812° |
| revolutions per day: | 14.12442974 |
| mean anomaly at epoch: | 255.2644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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