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 26073.61028314 +.00000000 +00000-0 +11790-3 0 00001
2 23342 97.6710 95.6481 0001925 74.6405 285.5023 14.84953275 05
| Epoch (UTC): | 14 March 2026 14:38:48 |
| Eccentricity: | 0.0001925 |
| inclination: | 97.6710° |
| perigee height: | 612 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 95.6481° |
| argument of perigee: | 74.6405° |
| revolutions per day: | 14.84953275 |
| mean anomaly at epoch: | 285.5023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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