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 12443U 26074.26216777 +.00000000 +00000-0 +80966-4 0 00007
2 12443 74.0515 81.1817 0003018 122.8381 237.3063 14.36035056 08
| Epoch (UTC): | 15 March 2026 06:17:31 |
| Eccentricity: | 0.0003018 |
| inclination: | 74.0515° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 81.1817° |
| argument of perigee: | 122.8381° |
| revolutions per day: | 14.36035056 |
| mean anomaly at epoch: | 237.3063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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