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 26071.79035411 +.00000000 +00000-0 +63202-4 0 00005
2 16327 82.5369 346.7537 0016624 256.0113 157.7628 14.85818270 06
| Epoch (UTC): | 12 March 2026 18:58:06 |
| Eccentricity: | 0.0016624 |
| inclination: | 82.5369° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 346.7537° |
| argument of perigee: | 256.0113° |
| revolutions per day: | 14.85818270 |
| mean anomaly at epoch: | 157.7628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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