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 18476U 26088.06438441 +.00000000 +00000-0 +11971-3 0 00005
2 18476 70.9894 322.9821 0207651 167.6665 342.4193 13.73206469 07
| Epoch (UTC): | 29 March 2026 01:32:42 |
| Eccentricity: | 0.0207651 |
| inclination: | 70.9894° |
| perigee height: | 835 km |
| apogee height: | 1141 km |
| right ascension of ascending node: | 322.9821° |
| argument of perigee: | 167.6665° |
| revolutions per day: | 13.73206469 |
| mean anomaly at epoch: | 342.4193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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