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 67803U 26145.46653170 +.00000000 +00000-0 +72359-3 0 00006
2 67803 97.2875 333.5057 0002033 82.9177 277.2297 15.33462693 00
| Epoch (UTC): | 25 May 2026 11:11:48 |
| Eccentricity: | 0.0002033 |
| inclination: | 97.2875° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5057° |
| argument of perigee: | 82.9177° |
| revolutions per day: | 15.33462693 |
| mean anomaly at epoch: | 277.2297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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