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 23342U 26041.06324617 +.00000000 +00000-0 +10895-3 0 00005
2 23342 97.6735 64.3058 0002006 104.2223 255.9215 14.84888887 04
| Epoch (UTC): | 10 February 2026 01:31:04 |
| Eccentricity: | 0.0002006 |
| inclination: | 97.6735° |
| perigee height: | 613 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 64.3058° |
| argument of perigee: | 104.2223° |
| revolutions per day: | 14.84888887 |
| mean anomaly at epoch: | 255.9215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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