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 67814U 26145.06412229 +.00000000 +00000-0 +41054-3 0 00000
2 67814 97.2856 333.1321 0001394 90.6835 269.4567 15.33452475 07
| Epoch (UTC): | 25 May 2026 01:32:20 |
| Eccentricity: | 0.0001394 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 333.1321° |
| argument of perigee: | 90.6835° |
| revolutions per day: | 15.33452475 |
| mean anomaly at epoch: | 269.4567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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