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 26070U 26088.15899652 +.00000000 +00000-0 +19049-3 0 00003
2 26070 71.0022 56.8960 0015702 159.3680 200.8080 14.15827468 04
| Epoch (UTC): | 29 March 2026 03:48:57 |
| Eccentricity: | 0.0015702 |
| inclination: | 71.0022° |
| perigee height: | 828 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 56.8960° |
| argument of perigee: | 159.3680° |
| revolutions per day: | 14.15827468 |
| mean anomaly at epoch: | 200.8080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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