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 27473U 26067.00716159 +.00000000 +00000-0 -47900-3 0 00000
2 27473 63.4176 76.0382 0626308 348.0654 34.9275 12.01429410 07
| Epoch (UTC): | 08 March 2026 00:10:18 |
| Eccentricity: | 0.0626308 |
| inclination: | 63.4176° |
| perigee height: | 1170 km |
| apogee height: | 2179 km |
| right ascension of ascending node: | 76.0382° |
| argument of perigee: | 348.0654° |
| revolutions per day: | 12.01429410 |
| mean anomaly at epoch: | 34.9275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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