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 11111U 26088.17679042 +.00000000 +00000-0 +62646-4 0 00006
2 11111 74.0247 121.8287 0017608 256.3612 103.5580 14.35230576 05
| Epoch (UTC): | 29 March 2026 04:14:34 |
| Eccentricity: | 0.0017608 |
| inclination: | 74.0247° |
| perigee height: | 762 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 121.8287° |
| argument of perigee: | 256.3612° |
| revolutions per day: | 14.35230576 |
| mean anomaly at epoch: | 103.5580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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