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 27465U 26065.91580259 +.00000000 +00000-0 +77682-4 0 00009
2 27465 82.4812 45.4702 0027278 114.9080 245.4840 12.44943105 02
| Epoch (UTC): | 06 March 2026 21:58:45 |
| Eccentricity: | 0.0027278 |
| inclination: | 82.4812° |
| perigee height: | 1464 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 45.4702° |
| argument of perigee: | 114.9080° |
| revolutions per day: | 12.44943105 |
| mean anomaly at epoch: | 245.4840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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