▸Orbital parameters

Orbit class	SSO
Inclination	97.3842°
Eccentricity	0.0005678
Period	92.4 min
Apogee	395 km
Perigee	388 km
Mean motion	15.58709212 rev/day
RAAN	272.8007°
Arg of perigee	224.8181°
Mean anomaly	135.2617°
B*	1.6001e-3
Rev at epoch	8,215

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62636U 25009AD 26187.71124117 .00124758 00000-0 16001-2 0 9994

2 62636 97.3842 272.8007 0005678 224.8181 135.2617 15.58709212 82157

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4G-20",
  "OBJECT_ID": "2025-009AD",
  "EPOCH": "2026-07-06T17:04:11.237+00:00",
  "MEAN_MOTION": 15.58709212,
  "ECCENTRICITY": 0.0005678,
  "INCLINATION": 97.3842,
  "RA_OF_ASC_NODE": 272.8007,
  "ARG_OF_PERICENTER": 224.8181,
  "MEAN_ANOMALY": 135.2617,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62636,
  "REV_AT_EPOCH": 8215,
  "BSTAR": 0.0016001,
  "MEAN_MOTION_DOT": 0.00124758,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FLOCK 4G-20
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/62636

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.