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 67699U 26145.26478487 +.00000000 +00000-0 +53408-3 0 00007
2 67699 97.2825 256.8125 0000657 80.0391 280.0926 15.33460322 06
| Epoch (UTC): | 25 May 2026 06:21:17 |
| Eccentricity: | 0.0000657 |
| inclination: | 97.2825° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.8125° |
| argument of perigee: | 80.0391° |
| revolutions per day: | 15.33460322 |
| mean anomaly at epoch: | 280.0926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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