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 37839U 26088.11942576 +.00000000 +00000-0 +10918-3 0 00004
2 37839 19.9611 74.8547 0018340 272.1328 159.2115 14.13748926 04
| Epoch (UTC): | 29 March 2026 02:51:58 |
| Eccentricity: | 0.0018340 |
| inclination: | 19.9611° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 74.8547° |
| argument of perigee: | 272.1328° |
| revolutions per day: | 14.13748926 |
| mean anomaly at epoch: | 159.2115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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