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 67853U 26145.55078480 +.00000000 +00000-0 +33922-3 0 00009
2 67853 53.1583 207.2180 0001257 68.2478 291.8656 15.30201728 02
| Epoch (UTC): | 25 May 2026 13:13:07 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.2180° |
| argument of perigee: | 68.2478° |
| revolutions per day: | 15.30201728 |
| mean anomaly at epoch: | 291.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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