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 48373U 26145.29868479 +.00000000 +00000-0 +75695-4 0 00005
2 48373 53.1599 349.1761 0001184 63.7023 296.4100 15.31710528 00
| Epoch (UTC): | 25 May 2026 07:10:06 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 349.1761° |
| argument of perigee: | 63.7023° |
| revolutions per day: | 15.31710528 |
| mean anomaly at epoch: | 296.4100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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