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 08026U 26088.12730596 +.00000000 +00000-0 +83820-4 0 00001
2 08026 81.2756 100.9852 0023666 87.0715 273.3164 14.10800036 02
| Epoch (UTC): | 29 March 2026 03:03:19 |
| Eccentricity: | 0.0023666 |
| inclination: | 81.2756° |
| perigee height: | 840 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 100.9852° |
| argument of perigee: | 87.0715° |
| revolutions per day: | 14.10800036 |
| mean anomaly at epoch: | 273.3164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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