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 05104U 26106.68492573 +.00000000 +00000-0 +10967-3 0 00008
2 05104 88.1668 326.1839 0042209 266.5401 156.3198 12.67885072 01
| Epoch (UTC): | 16 April 2026 16:26:17 |
| Eccentricity: | 0.0042209 |
| inclination: | 88.1668° |
| perigee height: | 1358 km |
| apogee height: | 1423 km |
| right ascension of ascending node: | 326.1839° |
| argument of perigee: | 266.5401° |
| revolutions per day: | 12.67885072 |
| mean anomaly at epoch: | 156.3198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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