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 48376U 26145.66668980 +.00000000 +00000-0 +26115-3 0 00006
2 48376 53.1602 349.0933 0001387 99.4302 342.1389 15.46803274 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.1602° |
| perigee height: | 425 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 349.0933° |
| argument of perigee: | 99.4302° |
| revolutions per day: | 15.46803274 |
| mean anomaly at epoch: | 342.1389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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