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 67854U 26145.34112185 +.00000000 +00000-0 +41262-3 0 00004
2 67854 53.1577 208.0405 0001146 85.4376 274.6756 15.30204977 09
| Epoch (UTC): | 25 May 2026 08:11:12 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 208.0405° |
| argument of perigee: | 85.4376° |
| revolutions per day: | 15.30204977 |
| mean anomaly at epoch: | 274.6756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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