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 44078U 26145.48074955 +.00000000 +00000-0 +13371-3 0 00004
2 44078 98.4657 204.4040 0017299 287.5963 72.3338 14.43675536 06
| Epoch (UTC): | 25 May 2026 11:32:16 |
| Eccentricity: | 0.0017299 |
| inclination: | 98.4657° |
| perigee height: | 734 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 204.4040° |
| argument of perigee: | 287.5963° |
| revolutions per day: | 14.43675536 |
| mean anomaly at epoch: | 72.3338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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