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 30794U 26145.31742984 +.00000000 +00000-0 +00000-0 0 00002
2 30794 5.2438 74.0124 0004001 356.8170 21.5864 1.00272801 07
| Epoch (UTC): | 25 May 2026 07:37:05 |
| Eccentricity: | 0.0004001 |
| inclination: | 5.2438° |
| perigee height: | 35769 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 74.0124° |
| argument of perigee: | 356.8170° |
| revolutions per day: | 1.00272801 |
| mean anomaly at epoch: | 21.5864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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