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 08132U 26121.87261191 +.00000000 +00000-0 +00000-0 0 00004
2 08132 4.1573 275.1861 0005434 59.6779 355.6017 0.99985288 00
| Epoch (UTC): | 01 May 2026 20:56:33 |
| Eccentricity: | 0.0005434 |
| inclination: | 4.1573° |
| perigee height: | 35844 km |
| apogee height: | 35890 km |
| right ascension of ascending node: | 275.1861° |
| argument of perigee: | 59.6779° |
| revolutions per day: | 0.99985288 |
| mean anomaly at epoch: | 355.6017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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