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 16910U 26088.00952218 +.00000000 +00000-0 +23407-3 0 00000
2 16910 50.0047 297.8346 0072977 72.1127 91.8813 12.32655336 02
| Epoch (UTC): | 29 March 2026 00:13:42 |
| Eccentricity: | 0.0072977 |
| inclination: | 50.0047° |
| perigee height: | 1480 km |
| apogee height: | 1596 km |
| right ascension of ascending node: | 297.8346° |
| argument of perigee: | 72.1127° |
| revolutions per day: | 12.32655336 |
| mean anomaly at epoch: | 91.8813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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