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 26536U 26088.12957895 +.00000000 +00000-0 +93540-4 0 00000
2 26536 98.4685 106.6182 0010690 165.1018 195.0473 14.13903614 07
| Epoch (UTC): | 29 March 2026 03:06:35 |
| Eccentricity: | 0.0010690 |
| inclination: | 98.4685° |
| perigee height: | 838 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 106.6182° |
| argument of perigee: | 165.1018° |
| revolutions per day: | 14.13903614 |
| mean anomaly at epoch: | 195.0473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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