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 21688U 26100.05145205 +.00000000 +00000-0 -60199-4 0 00009
2 21688 99.4143 106.2951 0024168 186.5384 241.2461 13.97867345 00
| Epoch (UTC): | 10 April 2026 01:14:05 |
| Eccentricity: | 0.0024168 |
| inclination: | 99.4143° |
| perigee height: | 884 km |
| apogee height: | 919 km |
| right ascension of ascending node: | 106.2951° |
| argument of perigee: | 186.5384° |
| revolutions per day: | 13.97867345 |
| mean anomaly at epoch: | 241.2461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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