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 05707U 26135.30434027 +.00000000 +00000-0 +37393-4 0 00001
2 05707 74.0263 197.7012 0024184 194.7174 165.3280 14.40492319 04
| Epoch (UTC): | 15 May 2026 07:18:14 |
| Eccentricity: | 0.0024184 |
| inclination: | 74.0263° |
| perigee height: | 740 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 197.7012° |
| argument of perigee: | 194.7174° |
| revolutions per day: | 14.40492319 |
| mean anomaly at epoch: | 165.3280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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