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 01778U 26065.24557226 +.00000000 +00000-0 +91052-4 0 00009
2 01778 34.2589 12.7197 0739860 191.9614 166.2546 13.49741205 03
| Epoch (UTC): | 06 March 2026 05:53:37 |
| Eccentricity: | 0.0739860 |
| inclination: | 34.2589° |
| perigee height: | 522 km |
| apogee height: | 1625 km |
| right ascension of ascending node: | 12.7197° |
| argument of perigee: | 191.9614° |
| revolutions per day: | 13.49741205 |
| mean anomaly at epoch: | 166.2546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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