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 16327U 26067.57005375 +.00000000 +00000-0 +83863-4 0 00007
2 16327 82.5370 350.7132 0016581 271.3271 262.2955 14.85813332 00
| Epoch (UTC): | 08 March 2026 13:40:52 |
| Eccentricity: | 0.0016581 |
| inclination: | 82.5370° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 350.7132° |
| argument of perigee: | 271.3271° |
| revolutions per day: | 14.85813332 |
| mean anomaly at epoch: | 262.2955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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