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 67077U 26145.33464404 +.00000000 +00000-0 +19982-3 0 00008
2 67077 70.0012 181.3843 0003707 267.7560 92.3175 14.98335597 08
| Epoch (UTC): | 25 May 2026 08:01:53 |
| Eccentricity: | 0.0003707 |
| inclination: | 70.0012° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.3843° |
| argument of perigee: | 267.7560° |
| revolutions per day: | 14.98335597 |
| mean anomaly at epoch: | 92.3175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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