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 48301U 26145.24969574 +.00000000 +00000-0 +11546-4 0 00004
2 48301 53.1617 95.0925 0001282 85.0177 275.0971 15.31704561 06
| Epoch (UTC): | 25 May 2026 05:59:33 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.0925° |
| argument of perigee: | 85.0177° |
| revolutions per day: | 15.31704561 |
| mean anomaly at epoch: | 275.0971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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