▸Orbital parameters

Orbit class	SSO
Inclination	97.3914°
Eccentricity	0.0003006
Period	94.1 min
Apogee	479 km
Perigee	475 km
Mean motion	15.29723998 rev/day
RAAN	269.2176°
Arg of perigee	249.1867°
Mean anomaly	110.9051°
B*	2.7006e-4
Rev at epoch	13,959

▸Two-line element set (TLE)

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

1 62670U 25009BP 26188.18560823 .00007702 00000-0 27006-3 0 9999

2 62670 97.3914 269.2176 0003006 249.1867 110.9051 15.29723998139594

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4G-10",
  "OBJECT_ID": "2025-009BP",
  "EPOCH": "2026-07-07T04:27:16.551+00:00",
  "MEAN_MOTION": 15.29723998,
  "ECCENTRICITY": 0.0003006,
  "INCLINATION": 97.3914,
  "RA_OF_ASC_NODE": 269.2176,
  "ARG_OF_PERICENTER": 249.1867,
  "MEAN_ANOMALY": 110.9051,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62670,
  "REV_AT_EPOCH": 13959,
  "BSTAR": 0.00027006,
  "MEAN_MOTION_DOT": 0.00007702,
  "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-10
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/62670

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