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 43215U 26153.22077073 +.00000000 +00000-0 +11867-3 0 00009
2 43215 97.4445 160.8196 0001751 89.3127 270.8308 15.19160316 06
| Epoch (UTC): | 02 June 2026 05:17:54 |
| Eccentricity: | 0.0001751 |
| inclination: | 97.4445° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 160.8196° |
| argument of perigee: | 89.3127° |
| revolutions per day: | 15.19160316 |
| mean anomaly at epoch: | 270.8308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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