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 25114U 26150.33287447 +.00000000 +00000-0 +39759-3 0 00004
2 25114 45.0120 143.8491 0004868 207.2030 152.8567 14.46656983 03
| Epoch (UTC): | 30 May 2026 07:59:20 |
| Eccentricity: | 0.0004868 |
| inclination: | 45.0120° |
| perigee height: | 733 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 143.8491° |
| argument of perigee: | 207.2030° |
| revolutions per day: | 14.46656983 |
| mean anomaly at epoch: | 152.8567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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