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 28909U 26104.17265399 +.00000000 +00000-0 -11358-3 0 00008
2 28909 82.4735 351.1855 0007426 312.8669 202.6069 12.55289566 05
| Epoch (UTC): | 14 April 2026 04:08:37 |
| Eccentricity: | 0.0007426 |
| inclination: | 82.4735° |
| perigee height: | 1437 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 351.1855° |
| argument of perigee: | 312.8669° |
| revolutions per day: | 12.55289566 |
| mean anomaly at epoch: | 202.6069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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