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 23465U 26088.04398748 +.00000000 +00000-0 +42662-4 0 00004
2 23465 82.9228 82.4115 0038244 32.2751 26.5422 13.72021384 07
| Epoch (UTC): | 29 March 2026 01:03:20 |
| Eccentricity: | 0.0038244 |
| inclination: | 82.9228° |
| perigee height: | 964 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 82.4115° |
| argument of perigee: | 32.2751° |
| revolutions per day: | 13.72021384 |
| mean anomaly at epoch: | 26.5422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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