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 63167U 26145.61475859 +.00000000 +00000-0 -83274-5 0 00009
2 63167 88.9688 302.8854 0015004 15.8508 344.3110 13.51013404 07
| Epoch (UTC): | 25 May 2026 14:45:15 |
| Eccentricity: | 0.0015004 |
| inclination: | 88.9688° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 302.8854° |
| argument of perigee: | 15.8508° |
| revolutions per day: | 13.51013404 |
| mean anomaly at epoch: | 344.3110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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