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 26154.30368998 +.00000000 +00000-0 +65460-4 0 00007
2 16909 50.0129 196.0439 0011171 126.1859 319.6546 12.44486398 02
| Epoch (UTC): | 03 June 2026 07:17:18 |
| Eccentricity: | 0.0011171 |
| inclination: | 50.0129° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 196.0439° |
| argument of perigee: | 126.1859° |
| revolutions per day: | 12.44486398 |
| mean anomaly at epoch: | 319.6546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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