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 26580U 26145.34746512 +.00000000 +00000-0 +00000-0 0 00004
2 26580 0.1139 79.8161 0003555 347.0948 166.0618 1.00271039 03
| Epoch (UTC): | 25 May 2026 08:20:20 |
| Eccentricity: | 0.0003555 |
| inclination: | 0.1139° |
| perigee height: | 35772 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 79.8161° |
| argument of perigee: | 347.0948° |
| revolutions per day: | 1.00271039 |
| mean anomaly at epoch: | 166.0618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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