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 25019U 26161.14836249 +.00000000 +00000-0 +00000-0 0 00003
2 25019 12.7755 21.7732 0003412 338.4457 199.4963 1.00270197 00
| Epoch (UTC): | 10 June 2026 03:33:38 |
| Eccentricity: | 0.0003412 |
| inclination: | 12.7755° |
| perigee height: | 35773 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 21.7732° |
| argument of perigee: | 338.4457° |
| revolutions per day: | 1.00270197 |
| mean anomaly at epoch: | 199.4963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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