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 26107.07988477 +.00000000 +00000-0 +99772-4 0 00000
2 01804 79.8000 328.6695 1330783 356.4674 2.7657 12.28307062 06
| Epoch (UTC): | 17 April 2026 01:55:02 |
| Eccentricity: | 0.1330783 |
| inclination: | 79.8000° |
| perigee height: | 501 km |
| apogee height: | 2613 km |
| right ascension of ascending node: | 328.6695° |
| argument of perigee: | 356.4674° |
| revolutions per day: | 12.28307062 |
| mean anomaly at epoch: | 2.7657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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