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 16909U 26053.26244500 +.00000000 +00000-0 +14734-3 0 00009
2 16909 50.0146 146.6864 0011079 228.3944 160.6669 12.44485550 00
| Epoch (UTC): | 22 February 2026 06:17:55 |
| Eccentricity: | 0.0011079 |
| inclination: | 50.0146° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 146.6864° |
| argument of perigee: | 228.3944° |
| revolutions per day: | 12.44485550 |
| mean anomaly at epoch: | 160.6669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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