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 48051U 26145.48494858 +.00000000 +00000-0 +87700-3 0 00004
2 48051 87.8950 324.7298 0001545 93.4417 266.6889 13.13468692 03
| Epoch (UTC): | 25 May 2026 11:38:19 |
| Eccentricity: | 0.0001545 |
| inclination: | 87.8950° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7298° |
| argument of perigee: | 93.4417° |
| revolutions per day: | 13.13468692 |
| mean anomaly at epoch: | 266.6889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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