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 38340U 26106.29142900 +.00000000 +00000-0 +19895-3 0 00008
2 38340 98.2076 236.7470 0008509 33.2188 326.9562 14.90689635 02
| Epoch (UTC): | 16 April 2026 06:59:39 |
| Eccentricity: | 0.0008509 |
| inclination: | 98.2076° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 236.7470° |
| argument of perigee: | 33.2188° |
| revolutions per day: | 14.90689635 |
| mean anomaly at epoch: | 326.9562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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