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 26150.55936205 +.00000000 +00000-0 +10544-3 0 00003
2 23342 97.6628 169.7163 0002060 103.9247 256.2197 14.85061442 08
| Epoch (UTC): | 30 May 2026 13:25:28 |
| Eccentricity: | 0.0002060 |
| inclination: | 97.6628° |
| perigee height: | 612 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 169.7163° |
| argument of perigee: | 103.9247° |
| revolutions per day: | 14.85061442 |
| mean anomaly at epoch: | 256.2197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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