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 25158U 26088.18908700 +.00000000 +00000-0 +46439-3 0 00000
2 25158 107.9615 1.4051 0042616 109.7993 250.7749 14.35347862 07
| Epoch (UTC): | 29 March 2026 04:32:17 |
| Eccentricity: | 0.0042616 |
| inclination: | 107.9615° |
| perigee height: | 743 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 1.4051° |
| argument of perigee: | 109.7993° |
| revolutions per day: | 14.35347862 |
| mean anomaly at epoch: | 250.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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