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 48121U 26145.46137939 +.00000000 +00000-0 +14585-4 0 00006
2 48121 53.1589 157.8731 0001209 87.3883 272.7257 15.31704312 09
| Epoch (UTC): | 25 May 2026 11:04:23 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 157.8731° |
| argument of perigee: | 87.3883° |
| revolutions per day: | 15.31704312 |
| mean anomaly at epoch: | 272.7257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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