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 40025U 26049.57230550 +.00000000 +00000-0 +44388-3 0 00002
2 40025 98.0993 52.5718 0007058 273.5102 86.5322 15.16073923 02
| Epoch (UTC): | 18 February 2026 13:44:07 |
| Eccentricity: | 0.0007058 |
| inclination: | 98.0993° |
| perigee height: | 513 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 52.5718° |
| argument of perigee: | 273.5102° |
| revolutions per day: | 15.16073923 |
| mean anomaly at epoch: | 86.5322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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