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 07434U 26100.06580470 +.00000000 +00000-0 +80615-4 0 00004
2 07434 74.0458 58.5223 0021604 254.0956 105.7817 14.38206639 08
| Epoch (UTC): | 10 April 2026 01:34:45 |
| Eccentricity: | 0.0021604 |
| inclination: | 74.0458° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 58.5223° |
| argument of perigee: | 254.0956° |
| revolutions per day: | 14.38206639 |
| mean anomaly at epoch: | 105.7817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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