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 67874U 26145.44672205 +.00000000 +00000-0 +55077-3 0 00000
2 67874 53.1575 205.8603 0001043 56.9877 303.1225 15.34412880 06
| Epoch (UTC): | 25 May 2026 10:43:16 |
| Eccentricity: | 0.0001043 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 205.8603° |
| argument of perigee: | 56.9877° |
| revolutions per day: | 15.34412880 |
| mean anomaly at epoch: | 303.1225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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