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 67703U 26145.56113935 +.00000000 +00000-0 +73610-3 0 00007
2 67703 97.2852 257.1705 0000621 97.1389 262.9925 15.33484027 03
| Epoch (UTC): | 25 May 2026 13:28:02 |
| Eccentricity: | 0.0000621 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1705° |
| argument of perigee: | 97.1389° |
| revolutions per day: | 15.33484027 |
| mean anomaly at epoch: | 262.9925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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