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 63694U 26145.56425628 +.00000000 +00000-0 +99100-4 0 00000
2 63694 86.5023 320.7011 0001443 80.5457 279.5840 13.24409648 05
| Epoch (UTC): | 25 May 2026 13:32:31 |
| Eccentricity: | 0.0001443 |
| inclination: | 86.5023° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.7011° |
| argument of perigee: | 80.5457° |
| revolutions per day: | 13.24409648 |
| mean anomaly at epoch: | 279.5840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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