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 00050U 26048.38207046 +.00000000 +00000-0 +94737-4 0 00002
2 00050 47.2291 173.5954 0113013 17.9409 342.5323 12.20162812 02
| Epoch (UTC): | 17 February 2026 09:10:10 |
| Eccentricity: | 0.0113013 |
| inclination: | 47.2291° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 173.5954° |
| argument of perigee: | 17.9409° |
| revolutions per day: | 12.20162812 |
| mean anomaly at epoch: | 342.5323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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