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 01804U 26140.87849271 +.00000000 +00000-0 +54730-4 0 00008
2 01804 79.7999 299.8996 1330065 287.9402 58.1308 12.28322917 09
| Epoch (UTC): | 20 May 2026 21:05:01 |
| Eccentricity: | 0.1330065 |
| inclination: | 79.7999° |
| perigee height: | 501 km |
| apogee height: | 2612 km |
| right ascension of ascending node: | 299.8996° |
| argument of perigee: | 287.9402° |
| revolutions per day: | 12.28322917 |
| mean anomaly at epoch: | 58.1308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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