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 67252U 26145.46616258 +.00000000 +00000-0 +29576-3 0 00003
2 67252 97.3947 220.7683 0011449 70.3066 289.9405 15.23896396 01
| Epoch (UTC): | 25 May 2026 11:11:16 |
| Eccentricity: | 0.0011449 |
| inclination: | 97.3947° |
| perigee height: | 486 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 220.7683° |
| argument of perigee: | 70.3066° |
| revolutions per day: | 15.23896396 |
| mean anomaly at epoch: | 289.9405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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