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 67534U 26145.43485244 +.00000000 +00000-0 +51983-3 0 00009
2 67534 97.2872 32.4593 0001412 85.8284 274.3120 15.33458536 03
| Epoch (UTC): | 25 May 2026 10:26:11 |
| Eccentricity: | 0.0001412 |
| inclination: | 97.2872° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.4593° |
| argument of perigee: | 85.8284° |
| revolutions per day: | 15.33458536 |
| mean anomaly at epoch: | 274.3120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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