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 17974U 26065.29307005 +.00000000 +00000-0 -21185-4 0 00008
2 17974 71.0084 39.9875 0015232 217.8495 246.2501 14.17641449 01
| Epoch (UTC): | 06 March 2026 07:02:01 |
| Eccentricity: | 0.0015232 |
| inclination: | 71.0084° |
| perigee height: | 822 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 39.9875° |
| argument of perigee: | 217.8495° |
| revolutions per day: | 14.17641449 |
| mean anomaly at epoch: | 246.2501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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