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 42259U 26088.03878272 +.00000000 +00000-0 +12237-2 0 00003
2 42259 98.6374 122.6859 0011587 149.4270 210.7594 14.36584987 06
| Epoch (UTC): | 29 March 2026 00:55:50 |
| Eccentricity: | 0.0011587 |
| inclination: | 98.6374° |
| perigee height: | 762 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 122.6859° |
| argument of perigee: | 149.4270° |
| revolutions per day: | 14.36584987 |
| mean anomaly at epoch: | 210.7594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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