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 63169U 26145.59892372 +.00000000 +00000-0 +10011-3 0 00007
2 63169 88.9693 302.3843 0013626 359.7677 0.3472 13.62036379 01
| Epoch (UTC): | 25 May 2026 14:22:27 |
| Eccentricity: | 0.0013626 |
| inclination: | 88.9693° |
| perigee height: | 1018 km |
| apogee height: | 1038 km |
| right ascension of ascending node: | 302.3843° |
| argument of perigee: | 359.7677° |
| revolutions per day: | 13.62036379 |
| mean anomaly at epoch: | 0.3472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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