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 26045.94216271 +.00000000 +00000-0 +44757-3 0 00003
2 40025 98.0999 48.7002 0007118 289.1859 70.8601 15.15999266 02
| Epoch (UTC): | 14 February 2026 22:36:42 |
| Eccentricity: | 0.0007118 |
| inclination: | 98.0999° |
| perigee height: | 513 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 48.7002° |
| argument of perigee: | 289.1859° |
| revolutions per day: | 15.15999266 |
| mean anomaly at epoch: | 70.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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