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 00022U 26088.16370519 +.00000000 +00000-0 +51265-3 0 00005
2 00022 50.2413 135.3611 0079909 161.8070 198.5778 15.27224593 03
| Epoch (UTC): | 29 March 2026 03:55:44 |
| Eccentricity: | 0.0079909 |
| inclination: | 50.2413° |
| perigee height: | 429 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 135.3611° |
| argument of perigee: | 161.8070° |
| revolutions per day: | 15.27224593 |
| mean anomaly at epoch: | 198.5778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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