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 21172U 26088.22848264 +.00000000 +00000-0 +20305-3 0 00009
2 21172 74.0353 45.4209 0132952 120.5555 354.2533 12.27723239 09
| Epoch (UTC): | 29 March 2026 05:29:00 |
| Eccentricity: | 0.0132952 |
| inclination: | 74.0353° |
| perigee height: | 1454 km |
| apogee height: | 1665 km |
| right ascension of ascending node: | 45.4209° |
| argument of perigee: | 120.5555° |
| revolutions per day: | 12.27723239 |
| mean anomaly at epoch: | 354.2533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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