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 67085U 26145.36784679 +.00000000 +00000-0 +21673-3 0 00009
2 67085 70.0008 181.1028 0003671 268.1618 91.9121 14.98336159 05
| Epoch (UTC): | 25 May 2026 08:49:41 |
| Eccentricity: | 0.0003671 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.1028° |
| argument of perigee: | 268.1618° |
| revolutions per day: | 14.98336159 |
| mean anomaly at epoch: | 91.9121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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