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 29270U 26145.59031513 +.00000000 +00000-0 +00000-0 0 00008
2 29270 1.6054 82.4841 0003635 338.6326 67.6856 1.00275043 03
| Epoch (UTC): | 25 May 2026 14:10:03 |
| Eccentricity: | 0.0003635 |
| inclination: | 1.6054° |
| perigee height: | 35770 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 82.4841° |
| argument of perigee: | 338.6326° |
| revolutions per day: | 1.00275043 |
| mean anomaly at epoch: | 67.6856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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