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 25407U 26019.20056750 +.00000000 +00000-0 +18443-3 0 00007
2 25407 71.0117 285.6489 0005269 106.4315 253.7387 14.16182382 02
| Epoch (UTC): | 19 January 2026 04:48:49 |
| Eccentricity: | 0.0005269 |
| inclination: | 71.0117° |
| perigee height: | 834 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 285.6489° |
| argument of perigee: | 106.4315° |
| revolutions per day: | 14.16182382 |
| mean anomaly at epoch: | 253.7387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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