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 data is extracted from the following two-line orbital elements,
1 40263U 14059C 25312.74750502 .00024199 00000-0 27813-2 0 9995
2 40263 98.1920 53.7365 0061488 280.8413 78.5884 14.84413035590285
| Epoch (UTC): | 08 November 2025 17:56:24 |
| Eccentricity: | 0.0061488 |
| inclination: | 98.1920° |
| perigee height: | 572 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 53.7365° |
| argument of perigee: | 280.8413° |
| revolutions per day: | 14.84413035 |
| mean anomaly at epoch: | 78.5884° |
| orbit number at epoch: | 59028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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