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 48291U 26145.54518609 +.00000000 +00000-0 +32800-4 0 00000
2 48291 53.1606 80.3540 0001400 93.6298 266.4863 15.31704099 03
| Epoch (UTC): | 25 May 2026 13:05:04 |
| Eccentricity: | 0.0001400 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 80.3540° |
| argument of perigee: | 93.6298° |
| revolutions per day: | 15.31704099 |
| mean anomaly at epoch: | 266.4863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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