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 42299U 26070.67315667 +.00000000 +00000-0 +62969-2 0 00009
2 42299 98.6977 146.5143 0013398 219.8335 140.1895 14.85331833 00
| Epoch (UTC): | 11 March 2026 16:09:20 |
| Eccentricity: | 0.0013398 |
| inclination: | 98.6977° |
| perigee height: | 603 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 146.5143° |
| argument of perigee: | 219.8335° |
| revolutions per day: | 14.85331833 |
| mean anomaly at epoch: | 140.1895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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