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 16369U 26069.54496772 +.00000000 +00000-0 +76003-4 0 00005
2 16369 82.9378 136.7286 0035101 233.9790 241.5503 13.77179810 04
| Epoch (UTC): | 10 March 2026 13:04:45 |
| Eccentricity: | 0.0035101 |
| inclination: | 82.9378° |
| perigee height: | 948 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 136.7286° |
| argument of perigee: | 233.9790° |
| revolutions per day: | 13.77179810 |
| mean anomaly at epoch: | 241.5503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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