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 38248U 26150.19117889 +.00000000 +00000-0 +65323-3 0 00008
2 38248 97.4372 196.8995 0003229 157.5082 202.6320 15.64661643 07
| Epoch (UTC): | 30 May 2026 04:35:17 |
| Eccentricity: | 0.0003229 |
| inclination: | 97.4372° |
| perigee height: | 372 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 196.8995° |
| argument of perigee: | 157.5082° |
| revolutions per day: | 15.64661643 |
| mean anomaly at epoch: | 202.6320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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