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 26076.21758707 +.00000000 +00000-0 +10875-3 0 00000
2 16369 82.9364 131.7639 0035435 214.8491 203.8448 13.77181283 08
| Epoch (UTC): | 17 March 2026 05:13:19 |
| Eccentricity: | 0.0035435 |
| inclination: | 82.9364° |
| perigee height: | 948 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 131.7639° |
| argument of perigee: | 214.8491° |
| revolutions per day: | 13.77181283 |
| mean anomaly at epoch: | 203.8448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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