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 00446U 26053.74972476 +.00000000 +00000-0 -16800-5 0 00000
2 00446 50.1423 48.8182 0070178 35.7832 133.7538 13.35358953 08
| Epoch (UTC): | 22 February 2026 17:59:36 |
| Eccentricity: | 0.0070178 |
| inclination: | 50.1423° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 48.8182° |
| argument of perigee: | 35.7832° |
| revolutions per day: | 13.35358953 |
| mean anomaly at epoch: | 133.7538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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