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 43484U 26145.64122586 +.00000000 +00000-0 +63452-4 0 00002
2 43484 97.7766 209.1505 0010608 245.7329 114.2774 14.76600204 02
| Epoch (UTC): | 25 May 2026 15:23:21 |
| Eccentricity: | 0.0010608 |
| inclination: | 97.7766° |
| perigee height: | 633 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 209.1505° |
| argument of perigee: | 245.7329° |
| revolutions per day: | 14.76600204 |
| mean anomaly at epoch: | 114.2774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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