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 00020U 26038.21672891 +.00000000 +00000-0 +53323-3 0 00009
2 00020 33.3448 14.8669 1638324 76.8077 300.9500 11.61808111 00
| Epoch (UTC): | 07 February 2026 05:12:05 |
| Eccentricity: | 0.1638324 |
| inclination: | 33.3448° |
| perigee height: | 507 km |
| apogee height: | 3206 km |
| right ascension of ascending node: | 14.8669° |
| argument of perigee: | 76.8077° |
| revolutions per day: | 11.61808111 |
| mean anomaly at epoch: | 300.9500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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