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 26065.32142558 +.00000000 +00000-0 +10295-3 0 00007
2 16369 82.9385 139.8707 0034934 246.1704 181.5116 13.77179058 05
| Epoch (UTC): | 06 March 2026 07:42:51 |
| Eccentricity: | 0.0034934 |
| inclination: | 82.9385° |
| perigee height: | 948 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 139.8707° |
| argument of perigee: | 246.1704° |
| revolutions per day: | 13.77179058 |
| mean anomaly at epoch: | 181.5116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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