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 48621U 26145.59193086 +.00000000 +00000-0 +37364-3 0 00009
2 48621 66.0002 0.9552 0011354 271.9045 88.0723 13.83375206 06
| Epoch (UTC): | 25 May 2026 14:12:22 |
| Eccentricity: | 0.0011354 |
| inclination: | 66.0002° |
| perigee height: | 944 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 0.9552° |
| argument of perigee: | 271.9045° |
| revolutions per day: | 13.83375206 |
| mean anomaly at epoch: | 88.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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