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 08172U 26105.88957597 +.00000000 +00000-0 +88161-4 0 00001
2 08172 101.9826 123.3928 0052970 209.9433 221.2032 12.54929324 01
| Epoch (UTC): | 15 April 2026 21:20:59 |
| Eccentricity: | 0.0052970 |
| inclination: | 101.9826° |
| perigee height: | 1403 km |
| apogee height: | 1485 km |
| right ascension of ascending node: | 123.3928° |
| argument of perigee: | 209.9433° |
| revolutions per day: | 12.54929324 |
| mean anomaly at epoch: | 221.2032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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