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 03840U 26086.28840492 +.00000000 +00000-0 +26001-3 0 00009
2 03840 80.6082 36.3160 0034298 8.7211 144.8350 12.58661408 01
| Epoch (UTC): | 27 March 2026 06:55:18 |
| Eccentricity: | 0.0034298 |
| inclination: | 80.6082° |
| perigee height: | 1402 km |
| apogee height: | 1455 km |
| right ascension of ascending node: | 36.3160° |
| argument of perigee: | 8.7211° |
| revolutions per day: | 12.58661408 |
| mean anomaly at epoch: | 144.8350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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