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 16496U 26037.76426024 +.00000000 +00000-0 +10554-3 0 00006
2 16496 82.5270 288.8449 0077108 16.3601 344.0077 14.86772644 09
| Epoch (UTC): | 06 February 2026 18:20:32 |
| Eccentricity: | 0.0077108 |
| inclination: | 82.5270° |
| perigee height: | 554 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 288.8449° |
| argument of perigee: | 16.3601° |
| revolutions per day: | 14.86772644 |
| mean anomaly at epoch: | 344.0077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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