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 26088.18529014 +.00000000 +00000-0 +37494-3 0 00000
2 01804 79.8040 344.7396 1331025 34.7562 333.3557 12.28279456 06
| Epoch (UTC): | 29 March 2026 04:26:49 |
| Eccentricity: | 0.1331025 |
| inclination: | 79.8040° |
| perigee height: | 501 km |
| apogee height: | 2613 km |
| right ascension of ascending node: | 344.7396° |
| argument of perigee: | 34.7562° |
| revolutions per day: | 12.28279456 |
| mean anomaly at epoch: | 333.3557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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