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 26071.54716411 +.00000000 +00000-0 +55429-3 0 00007
2 40025 98.1010 76.0232 0008665 184.3820 175.7336 15.16587552 00
| Epoch (UTC): | 12 March 2026 13:07:54 |
| Eccentricity: | 0.0008665 |
| inclination: | 98.1010° |
| perigee height: | 510 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 76.0232° |
| argument of perigee: | 184.3820° |
| revolutions per day: | 15.16587552 |
| mean anomaly at epoch: | 175.7336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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