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 67710U 26145.24031426 +.00000000 +00000-0 +65938-3 0 00008
2 67710 97.2849 256.8466 0000676 44.5948 315.5349 15.33451973 03
| Epoch (UTC): | 25 May 2026 05:46:03 |
| Eccentricity: | 0.0000676 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.8466° |
| argument of perigee: | 44.5948° |
| revolutions per day: | 15.33451973 |
| mean anomaly at epoch: | 315.5349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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