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 26064.05276086 +.00000000 +00000-0 +91116-4 0 00002
2 23343 97.7114 95.0582 0005466 228.2670 160.2790 14.79401664 00
| Epoch (UTC): | 05 March 2026 01:15:58 |
| Eccentricity: | 0.0005466 |
| inclination: | 97.7114° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 95.0582° |
| argument of perigee: | 228.2670° |
| revolutions per day: | 14.79401664 |
| mean anomaly at epoch: | 160.2790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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