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 39189U 26144.77219698 +.00000000 +00000-0 +00000-0 0 00009
2 39189 0.0452 346.0512 0005135 70.2536 303.7435 5.00115261 07
| Epoch (UTC): | 24 May 2026 18:31:57 |
| Eccentricity: | 0.0005135 |
| inclination: | 0.0452° |
| perigee height: | 8058 km |
| apogee height: | 8073 km |
| right ascension of ascending node: | 346.0512° |
| argument of perigee: | 70.2536° |
| revolutions per day: | 5.00115261 |
| mean anomaly at epoch: | 303.7435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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