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 23343U 26067.10362042 +.00000000 +00000-0 +10076-3 0 00004
2 23343 97.7111 97.9855 0005664 216.4629 210.5776 14.79406268 02
| Epoch (UTC): | 08 March 2026 02:29:12 |
| Eccentricity: | 0.0005664 |
| inclination: | 97.7111° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 97.9855° |
| argument of perigee: | 216.4629° |
| revolutions per day: | 14.79406268 |
| mean anomaly at epoch: | 210.5776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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