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 26070.64262978 +.00000000 +00000-0 +80574-4 0 00005
2 16369 82.9376 135.9120 0035136 230.8031 283.6953 13.77180091 01
| Epoch (UTC): | 11 March 2026 15:25:23 |
| Eccentricity: | 0.0035136 |
| inclination: | 82.9376° |
| perigee height: | 948 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 135.9120° |
| argument of perigee: | 230.8031° |
| revolutions per day: | 13.77180091 |
| mean anomaly at epoch: | 283.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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