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 21228U 26074.02930593 +.00000000 +00000-0 +41636-3 0 00001
2 21228 23.9959 211.1348 1133299 213.1735 139.2380 12.55585681 06
| Epoch (UTC): | 15 March 2026 00:42:12 |
| Eccentricity: | 0.1133299 |
| inclination: | 23.9959° |
| perigee height: | 555 km |
| apogee height: | 2327 km |
| right ascension of ascending node: | 211.1348° |
| argument of perigee: | 213.1735° |
| revolutions per day: | 12.55585681 |
| mean anomaly at epoch: | 139.2380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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