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 38734U 26106.99107137 +.00000000 +00000-0 +10296-2 0 00000
2 38734 82.4691 103.1455 0016127 191.1931 168.8793 12.44900985 02
| Epoch (UTC): | 16 April 2026 23:47:08 |
| Eccentricity: | 0.0016127 |
| inclination: | 82.4691° |
| perigee height: | 1473 km |
| apogee height: | 1499 km |
| right ascension of ascending node: | 103.1455° |
| argument of perigee: | 191.1931° |
| revolutions per day: | 12.44900985 |
| mean anomaly at epoch: | 168.8793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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