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 26150.30806530 +.00000000 +00000-0 +00000-0 0 00005
2 30794 5.2564 73.9536 0004002 2.2983 17.7122 1.00270958 02
| Epoch (UTC): | 30 May 2026 07:23:36 |
| Eccentricity: | 0.0004002 |
| inclination: | 5.2564° |
| perigee height: | 35770 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 73.9536° |
| argument of perigee: | 2.2983° |
| revolutions per day: | 1.00270958 |
| mean anomaly at epoch: | 17.7122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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